• Title/Summary/Keyword: steel ball

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Impact Behavior Simulation of Anisotropic Materials (이방성 재료의 충격거동에 관한 시뮬레이션)

  • Ahn, Kook-Chan;Jung, Dae-Sik;Kim, Bong-Hwan
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.10 no.1
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    • pp.38-46
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    • 2011
  • A study was performed to investigate the dynamic behaviors of fiber-reinforced composite materials subjected to transversely low-velocity impact. For this purpose, the simulation of modified beam finite element based on higher order beam theory for two(isotropic and anisotropic) materials is carried out according to the changes of material property, stacking sequence, geometric dimension and impact velocity of steel ball, etc. Main composite materials for simulation are composed of $[0^{\circ}/90^{\circ}/0^{\circ}/-90^{\circ}/0^{\circ}]_{2s}$, $[0^{\circ}/90^{\circ}/0^{\circ}/-90^{\circ}/0^{\circ}]_s$ and $[0^{\circ}/45^{\circ}/0^{\circ}/-45^{\circ}/0^{\circ}]_{2s}$, $[0^{\circ}/45^{\circ}/0^{\circ}/-45^{\circ}/0^{\circ}]_s$ stacking sequences. The effectiveness of this simulation for qualitative and quantitative evaluations in composite materials subjected to foreign object impact was established.

A Study on the Impact Damage and Residual Bending Strength of CF/EPOXY Composite Laminate Plates Under High Temperature (고온분위기하에서 탄소섬유강화 복합재적층판의 충격손상과 잔류굽힘강도)

  • 양인영;박정수
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.8
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    • pp.1930-1938
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    • 1994
  • In this paper, the effects of temperature change on the impact of CFRP laminates was experimentally studied. Composite laminates used for this experiment are CFRP orthotropic laminated plates, which have two-interfaces$[0_6^{\circ}/90_7^{\circ}]_s$ and four-interfaces$[0_3^{\circ}/90_6^{\circ}/0_3^{\circ}]_s$. The interrelations between the impact energy vs. delamination area, the impact energy vs. residual bending strength, and the interlayer delamination area vs. the decrease of the residual flexural strength of carbon fiber epoxy composite laminates subjected to FOD(Foreign Object Damage) under high temperatures were experimentally observed.

미끄럼운동 시 TiN코팅에 형성되는 산화막이 마찰 및 마멸 특성에 미치는 영향

  • Jo, Jeong-U;Im, Jeong-Sun;U, Sang-Gyu;Lee, Yeong-Je
    • Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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    • 2002.05a
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    • pp.310-316
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    • 2002
  • In this study, the effects of oxide layer formed on the wear tracks of TiN coated silicon wafer on friction and wear characteristics were investigated. Silicon wafer was used for the substrate of coated disk specimens, which were prepared by depositing TiN coating with $1{\mu}m$ in coating thickness. AISI 52100 steel ball was used for the counterpart. The tests were performed both in air for forming oxide layer on the wear track and in nitrogen to avoid oxidation. This paper reports characterization of the oxide layer effects on friction and wear characteristics using X-ray diffraction (XRD). Auger electron spectroscopy (AES), scanning electron microscopy (SEM) and sliding tests.

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Wear behavior of SM55C steel by rolling contact (구름접촉에 의한 SM55C의 마멸 거동)

  • Park, Beom-Su;Chae, Young-Hun;Kim, Seock-Sam
    • Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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    • 2002.05a
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    • pp.240-247
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    • 2002
  • The rolling wear behavior of SM55C is investigated under lubrication. This is a comparative tribological behavior of heat treatment effect for SM55C. Rolling wear test method is used for Ball-on-disk type. Specimens can be classified into two main groups: as-annealing and non-annealing. As result of wear behavior, flanking initial time of non-annealing specimen keep at retard but it have not under high normal load. One of the notable features of annealing specimen is steady flanking initial time for a normal load in this experiment. Failure mechanism of SM55C is due to the fatigue wear such like flanking, pitting etc.. Flanking leads to abruptly fracture of worn surface. Fracture mechanism has a connection with normal load and polishing direction of specimens.

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A study on the evaluation method for slag detachability (SLAG 박리성 평가 방법에 대한 고찰)

  • 우유철;김희진
    • Journal of Welding and Joining
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    • v.5 no.1
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    • pp.57-63
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    • 1987
  • A method which can be used for evaluating slag detachability is proposed in this study. The proposed method was intended to get an absolute value for slag detachability, to give consistent value for a given welded joint, and finally to be simple to test. With a test fig made in this study, an impact by dropping a steel ball (13Kg in weight) is applied on the back side of an as-welded plate having a slag layer on the weld bead. Such impact applied forces the slag to drop off from the bead surface. In order to make a quantitative evaluation the amount of slag removed was measured with increasing the number of drops. Using this method six kinds of fluxes were evaluated in terms of the effects of flux type, basicity and weding variables on the slag detachability. As an initial result of this test, it was found that welding heat input affects the detachability significantly. Most importantly the evaluation made using the presently proposed method gives the same order of ranking as that of the actual practice done by a welder.

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A Study on Advanced Small Punch Test for Evaluation of Material Degradation in Weldment Microstructures (용접부 미세조직의 재질열화 평가를 위한 Advanced Small Punch 시험에 관한 연구)

  • 이동환;이송인;박종진;유효선
    • Journal of Welding and Joining
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    • v.21 no.1
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    • pp.99-106
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    • 2003
  • This research was aimed to evaluate the material degradation with various microstructures of X20CrMoV121 steel weldment by Advanced Small Punch(ASP) test. Due to the regional limitation on constitutive structures, the minimized loading ball(${\varphi}1.5mm$) and bore diameter of lower die(${\varphi}3mm$) were designed for the ASP test. The micro-hardness test was also performed to assess the mechanical properties with artificial aging heat treatment. Material degradation was estimated by ductile-brittle transition temperature(DBTT). The results obtained from the ASP test were compared with those from conventional small punch(CSP) test and CVN impact test for several weldment microstructures. It was found that the ASP test clearly showed the microstructural dependance on the material degradation in the weldment.

Wave Propagation of Laminated Composites by the Hgih-Velocity Impact Experiment (고속 충격실험에 의한 적층 복합재의 파동전파에 관한 연구)

  • 김문생;김남식;박승범
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.17 no.8
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    • pp.1931-1939
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    • 1993
  • The wave propagation characteristics of laminated composites subjected to a transverse high-velocity impact of a steel ball is investigated. For this purpose, high-velocity impact experiments were conducted to obtain the strain response histories, and a finite element analysis based on the higher-order shear deformation theory in conjunction with the static contact law is used. Test materials for investigation are glass/epoxy laminated composite materials with $[0^{\circ}/45^{\circ}/0^{\circ}/-45^{\circ}]_{2s}$ and $[90^{\circ}/-45^{\circ}/90^{\circ}-45^{\circ}/90^{\circ}]_{2s}$ stacking sequences. As a result, the strain responses obtained from the experiments represented the wave propagation characteristics in the transversely impact, also the wave propagation velocities obtained from high-velocity impact experiments and wave propagation theory agree well.

The Impact Stresses and Wave Propagation of Laminated Composites

  • Ahn, Kook Chan;Kim, Doo Hwan;Lee, Gwang Seok
    • International Journal of Safety
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    • v.1 no.1
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    • pp.7-12
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    • 2002
  • This paper demonstrates the impact stresses and wave propagation characteristics of glass/epoxy laminates subjected to the low-velocity impact by a steel ball theoretically and experimentally. A plate finite element model in conjunction with experimental contact laws is used for the theoretical investigation. The specimens for statical indentation and impact test are composed of $[0/45/0/-45/0]_28 and [90/45/90/-45/90]_28$ stacking sequences and have clamped-simply supported boundary conditions. Finally, these two results are compared and then the impulsive stress and wave propagation characteristics of this laminated composite are studied.

A Study on Wear Characteristics of High strength aluminum alloys by Surface Hardening (표면경화에 의한 고강도 알루미늄 합금의 마모 특성에 관한 연구)

  • Lee, Nam-Soo;Huh, Sun-Chul;Lee, Kwang-Young;Park, Won-Jo
    • Proceedings of the KSME Conference
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    • 2007.05a
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    • pp.1601-1606
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    • 2007
  • In order for high strength aluminum alloys to be used in transportation systems and the aerospace industry, excellent mechanical and physical properties are required. In particular, excellent anti-abrasion property is indispensable for parts that require driving force. In general, surface treatment technologies such as high frequency heat treatment, gas solid carburizing, surface rolling, shot peening are used as ways of improving anti-abrasion property. Among various surface treatment technologies, this research chose shot peening processing for Al7075-T6, which is well known as representative high-strength alloy steel. Wear characteristics were compared and analyzed after shot peening processing with shot ball velocities of 40m/s and 70m/s in order to investigate the effects of shot peening processing on wear characteristics.

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Characteristics for rotordynamics of laminated rotor supported by rolling bearings (구름베어링으로 지지된 적층로터의 로터다이나믹 특성)

  • Kim, Yeong-Chun;Park, Chul-Hyun;Park, Hei-Joo
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.11b
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    • pp.822-825
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    • 2002
  • A lot of rotating machinery are generally used in industrial field and the electrical machinery such as the motor and generator account for the most of the part. Generally motor and generator have electrical loss because of eddy current. So silicon steel sheets are used in order to reduce the electrical loss and furthermore laminated rotor is used for motor and generator to eliminate the electrical loss and heat generation. However, the more high speed, large scale and high precision of the system, the more important to estimate the critical speed. In this paper verifies the variation of the critical speeds in accordance with the variation of the pressing force of lamination plate for the rotor which is supported by ball bearing with the experimental data as well.

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